The GUNT Supersonic Wind Tunnel with Schlieren Optics is an advanced Eiffel-type open wind tunnel designed for studying aerodynamic properties of drag bodies under subsonic and supersonic conditions. It facilitates precise analysis of flow behavior at speeds up to Mach 1.8, including shock front visualization using Schlieren optics.
Product Features
- Designed for investigating subsonic and supersonic flow phenomena, crucial for gas turbines, jets, and rocket design
- Open wind tunnel with a fan drawing ambient air through the system
- Subsonic nozzle at air inlet with integrated flow straightener for uniform, low-turbulence velocity distribution
- Closed measuring section where air accelerates further and flows around drag bodies such as rockets, projectiles, and wedges
- Interchangeable walls in the measuring section allow generation of flow velocities up to Mach 1.8
- Supersonic and subsonic diffusers slow the airflow downstream before it passes through a suction filter to the fan
- Fan compresses air and emits it back to the environment; sound damper reduces noise at outlet
- Schlieren optics included for direct visualization of supersonic flow and shock fronts
- Pressure sensors detect flow pressures and transmit data via USB directly to a PC for software analysis
- Pressure also displayed on manometers at measuring points for real-time monitoring
- Continuous operation mode provides ample time for observation and data collection
Benefits
- Enables detailed study of compressible flow and supersonic aerodynamic effects
- Visualizes shock waves and flow discontinuities with Schlieren optics
- USB-connected sensors facilitate accurate, digital data acquisition and analysis
- Interchangeable components allow flexible adaptation for various experiment setups
- Quiet operation due to integrated sound damper enhances lab environment comfort
Why Choose the GUNT Supersonic Wind Tunnel?
The GUNT Supersonic Wind Tunnel with Schlieren Optics is ideal for advanced aerodynamic research and teaching, offering precise control and visualization of supersonic flows. Its modular design, digital data output, and high-speed capabilities make it essential for aerospace engineering and fluid dynamics studies.
